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- W2321824230 abstract "A two-dimensional, fully compressible. Navier-Stokes Computational Fluid Dynamic. (CFD) code is coupled with a Yave Optics (YO) propagation code to numerically predict the aerooptical performance of optical seniors located in ipen cavities onbosrd subsonic aircraft. The CFD code is used to define the aerodynamic flowfield surrounding the aeilsor initallation. The YO code uses the time-aver-Zed, ..~rriaLly varying density fields computed by the WJ code LO calculate the optical bias, blur, 8v.l Strehi ratio a t the sensor focal plana c a u 4 by the presence of the turbulent aerodynamic flowfield in the sensor'. field of view (FOV). Both code. are validated using aero-optical measurements made in a recent wind-tuonel test. The numerical resulrs agree extremely well with experimental data. The validated coder are used to study the scaling affects associated with rubrcale ground testing and t o analyze a full-scale flight test configuration for a variety of external flow conditions, sensor positions, sensor lines of sight (LOS), and cavity-blowing rates. The results of the parametric study indicate that the aerodynamic performance of the cavity and the aero-optical performance of the sensor in the cavity are both rtrong functions of the cavityblowing rates and sensor LOS and weak functions of the external flow and the sensor position." @default.
- W2321824230 created "2016-06-24" @default.
- W2321824230 creator A5009857402 @default.
- W2321824230 creator A5085902131 @default.
- W2321824230 date "1988-01-11" @default.
- W2321824230 modified "2023-09-23" @default.
- W2321824230 title "An integrated Navier-Stokes and wave optics numerical simulation technique for predicting the aero-optical performance about subsonic surveillance aircraft" @default.
- W2321824230 doi "https://doi.org/10.2514/6.1988-753" @default.
- W2321824230 hasPublicationYear "1988" @default.
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